View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 13260U 26088.04025897 +.00000000 +00000-0 -25676-4 0 00005
2 13260 65.8298 282.0007 0044006 302.5765 185.5519 13.74589429 09
| Epoch (UTC): | 29 March 2026 00:57:58 |
| Eccentricity: | 0.0044006 |
| inclination: | 65.8298° |
| perigee height: | 951 km |
| apogee height: | 1016 km |
| right ascension of ascending node: | 282.0007° |
| argument of perigee: | 302.5765° |
| revolutions per day: | 13.74589429 |
| mean anomaly at epoch: | 185.5519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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